ardupilot/ArduSub/land_detector.cpp

57 lines
1.5 KiB
C++
Raw Normal View History

/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
2016-01-14 15:30:56 -04:00
#include "Sub.h"
#define LAND_END_DEPTH -20 //Landed at 20cm depth
// counter to verify landings
static uint32_t land_detector_count = 0;
// run land and crash detectors
// called at MAIN_LOOP_RATE
2016-01-14 15:30:56 -04:00
void Sub::update_land_and_crash_detectors()
{
// update 1hz filtered acceleration
Vector3f accel_ef = ahrs.get_accel_ef_blended();
accel_ef.z += GRAVITY_MSS;
land_accel_ef_filter.apply(accel_ef, MAIN_LOOP_SECONDS);
update_land_detector();
crash_check();
}
// update_land_detector - checks if we have landed and updates the ap.land_complete flag
// called at MAIN_LOOP_RATE
2016-01-14 15:30:56 -04:00
void Sub::update_land_detector()
{
if(barometer.num_instances() > 1 && barometer.get_altitude() > LAND_END_DEPTH && ap.throttle_zero) {
set_land_complete(true);
} else {
set_land_complete(false);
}
}
2016-01-14 15:30:56 -04:00
void Sub::set_land_complete(bool b)
{
// if no change, exit immediately
if( ap.land_complete == b )
return;
land_detector_count = 0;
if(b){
Log_Write_Event(DATA_LAND_COMPLETE);
} else {
Log_Write_Event(DATA_NOT_LANDED);
}
ap.land_complete = b;
}
// update_throttle_thr_mix - sets motors throttle_low_comp value depending upon vehicle state
// low values favour pilot/autopilot throttle over attitude control, high values favour attitude control over throttle
// has no effect when throttle is above hover throttle
void Sub::update_throttle_thr_mix()
{
return; // placeholder, was used by heli only
}